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1. 发明公开

EP2154351A2 Inlet air conditioning system for a turbomachine 审中-公开
标题翻译： KlimaanlagefürEinlassluft einer Turbomaschine
公开(公告)号：EP2154351A2
公开(公告)日：2010-02-17
申请号：EP09167380.6
申请日：2009-08-06
申请人： General Electric Company
发明人： Chillar, Rahul J. , Rogers, David L. , Motakef, Abbas
IPC分类号： F02C7/04 , F02C7/143
CPC分类号： F02C7/143 , F02C7/04 , F02C7/057
摘要： An embodiment of the present invention provides an air conditioning system (115) located upstream of the inlet system (100) for a gas turbine. The air conditioning system (115) may comprise at least one conditioning module (145) for adjusting the temperature of the airstream. The at least one conditioning module (145) may have a plurality of forms including at least one of the following systems: a chiller, an evaporative cooler; a spray cooler, or combinations thereof The specific form of the at least one conditioning module (145) may be determined in part by the configuration of the gas turbine.
摘要翻译：本发明的实施例提供一种位于燃气轮机的入口系统（100）上游的空调系统（115）。空调系统（115）可以包括用于调节气流的温度的至少一个调节模块（145）。所述至少一个调节模块（145）可以具有包括以下系统中的至少一个的多个形式：冷却器，蒸发冷却器; 喷雾冷却器或其组合。至少一个调节模块（145）的特定形式可以部分地由燃气轮机的构造来确定。

2. 发明公开

EP2196651A3 Low grade heat recovery system for turbine air inlet 审中-公开
标题翻译：低品位热回收涡轮进气口
公开(公告)号：EP2196651A3
公开(公告)日：2011-07-06
申请号：EP09177612.0
申请日：2009-12-01
申请人： General Electric Company
发明人： Feher, Peter , Motakef, Abbas
IPC分类号： F02C7/047 , F02C7/08 , F01K23/10 , F02C6/18 , F02C7/143
CPC分类号： F02C7/08 , F01K23/10 , F02C7/047 , Y02E20/16
摘要： A heating and cooling system (100) for inlet air of a gas turbine engine (10) in a combined cycle power plant (80) having a steam turbine (90). The heating and cooling system (100) may include a fluid coil (110) positioned about the gas turbine engine (10), a heat exchanger (170) in communication with the fluid coil (110), and a condenser (180) in communication with the steam turbine (90) and the heat exchanger (170) such that waste heat from the steam turbine (90) is forwarded to the fluid coil (110).

3. 发明公开

EP2180165A3 A system and method for changing the efficiency of a combustion turbine 失效转让
标题翻译：系统和方法用于燃烧涡轮机效率的变化
公开(公告)号：EP2180165A3
公开(公告)日：2011-07-06
申请号：EP09173219.8
申请日：2009-10-16
申请人： General Electric Company
发明人： Feher, Peter , Motakef, Abbas
IPC分类号： F02C7/047 , F01K23/10 , F02C6/14 , F02C7/08 , F02C7/143
CPC分类号： F02C7/047 , F01K23/10 , F02C1/05 , F02C6/08
摘要： An embodiment of the present invention takes the form of an application and process that incorporates an external heat source (140) to increase the temperature of the airstream entering a compressor section (155) of a combustion turbine (150). An embodiment of the present invention may perform an anti-icing operation that may not require an Inlet Bleed Heat system (IBH) (125) to operate. An embodiment of the present invention may perform an anti-icing operation that may allow for the IGV angle to remain nearly constant. An embodiment of the present invention may increase the output and efficiency of a combustion turbine (150) operating at partload by delaying IBH operation and delaying the closing IGVs.

4. 发明公开

EP2196651A2 Low grade heat recovery system for turbine air inlet 审中-公开
标题翻译：低等级的Wärmerückgewinnungfür涡轮Lufteinlass
公开(公告)号：EP2196651A2
公开(公告)日：2010-06-16
申请号：EP09177612.0
申请日：2009-12-01
申请人： General Electric Company
发明人： Feher, Peter , Motakef, Abbas
IPC分类号： F02C7/047 , F02C7/08
CPC分类号： F02C7/08 , F01K23/10 , F02C7/047 , Y02E20/16
摘要： A heating and cooling system (100) for inlet air of a gas turbine engine (10) in a combined cycle power plant (80) having a steam turbine (90). The heating and cooling system (100) may include a fluid coil (110) positioned about the gas turbine engine (10), a heat exchanger (170) in communication with the fluid coil (110), and a condenser (180) in communication with the steam turbine (90) and the heat exchanger (170) such that waste heat from the steam turbine (90) is forwarded to the fluid coil (110).
摘要翻译：一种用于具有汽轮机（90）的联合循环动力装置（80）中的燃气涡轮发动机（10）的入口空气的加热和冷却系统（100）。加热和冷却系统（100）可以包括围绕燃气涡轮发动机（10）定位的流体盘管（110），与流体盘管（110）连通的热交换器（170），以及连通的冷凝器与蒸汽轮机（90）和热交换器（170）一起使得来自蒸汽涡轮（90）的废热被传送到流体盘管（110）。

5. 发明公开

EP2343437A1 Turbine inlet air heat pump-type system 审中-公开
标题翻译： Turbinen-Einlassluftwärmepumpensystem
公开(公告)号：EP2343437A1
公开(公告)日：2011-07-13
申请号：EP09177607.0
申请日：2009-12-01
申请人： General Electric Company
发明人： Motakef, Abbas , Feher, Peter
IPC分类号： F01K27/02 , F02C6/14 , F02C7/08 , F02C6/18
CPC分类号： F02C7/143 , F01K23/10 , F01K27/02 , F02C7/047 , Y02E20/14
摘要： A heating and cooling system (100) for inlet air of a turbine compressor (20). The heating and cooling system (100) may include a thermal energy storage tank charging loop (190), a cooling loop (200) in communication with the thermal energy storage charging loop (190), and a heating loop (210) in communication with the cooling loop (200) and the inlet air of the turbine compressor (20).
摘要翻译：一种用于涡轮压缩机（20）的入口空气的加热和冷却系统（100）。加热和冷却系统（100）可以包括与热能储存充电回路（190）连通的热能储存箱充电回路（190），冷却回路（200）以及与热能存储充电回路（190）连通的加热回路（210）冷却回路（200）和涡轮压缩机（20）的入口空气。

6. 发明公开

EP2196652A2 Gas turbine base load control by chilling modulation 审中-公开
标题翻译： Gasturbine Grundlast Kontrolle durch Modulation derKühlung
公开(公告)号：EP2196652A2
公开(公告)日：2010-06-16
申请号：EP09177606.2
申请日：2009-12-01
申请人： General Electric Company
发明人： Feher, Peter , Motakef, Abbas
IPC分类号： F02C7/057 , F02C7/143 , F02C9/16
CPC分类号： F02C7/057 , F02C7/143 , F02C9/16
摘要： A control system (100) for a base load output of a gas turbine engine. The control system (100) may include an inlet chilling coil system (210) for providing air to the gas turbine engine (110) at a desired temperature, a temperature control valve (260) in communication with the inlet chilling coil system (210), a temperature sensor (290) positioned about the gas turbine engine (110), and a temperature controller (270) in communication with the temperature control valve (260) and the temperature sensor (290). The temperature controller (270) modulates the temperature control valve (260) until the air provided to the gas turbine engine (110) by the inlet chilling coil system (210) reaches the desired temperature as sensed by the temperature sensor (290).
摘要翻译：一种用于燃气涡轮发动机的基本负载输出的控制系统（100）。控制系统（100）可以包括用于在期望温度下向燃气涡轮发动机（110）提供空气的入口冷却盘管系统（210），与入口冷却盘管系统（210）连通的温度控制阀（260），位于燃气涡轮发动机（110）周围的温度传感器（290）和与温度控制阀（260）和温度传感器（290）连通的温度控制器（270）。温度控制器（270）调节温度控制阀（260），直到由入口冷却盘管系统（210）提供到燃气涡轮发动机（110）的空气达到由温度传感器（290）感测到的期望温度。

7. 发明授权

EP2180165B1 A system and method for changing the efficiency of a combustion turbine 失效转让
公开(公告)号：EP2180165B1
公开(公告)日：2019-06-12
申请号：EP09173219.8
申请日：2009-10-16
申请人： General Electric Company
发明人： Feher, Peter , Motakef, Abbas
IPC分类号： F02C1/05 , F02C6/08 , F01K23/10 , F02C7/047

8. 发明公开

EP2620617A2 Combustion turbine inlet anti-icing resistive heating system 审中-公开
标题翻译： FrostbeständigesGasturbineneinlassheizsystem
公开(公告)号：EP2620617A2
公开(公告)日：2013-07-31
申请号：EP13152743.4
申请日：2013-01-25
申请人： General Electric Company
发明人： Scipio, Alston Ilford , Ekanayake, Sanji , Vu, Huong Van , Motakef, Abbas
IPC分类号： F02C7/047 , F02C7/052 , F02C7/055 , F02C7/057
CPC分类号： F02C7/047 , F02C7/052 , F02C7/055 , F02C7/057 , F05D2250/51
摘要： A resistive heating system for a combustion turbine susceptible to inlet air filter house component (42) and compressor icing includes a plurality of heating panels (bundles) (48) arranged in a substantially-planar array (46, 47), adapted to be located on or adjacent to the turbine's inlet air filter house (42). Each heating panel (48) is provided with one or more electrically-resistive heating elements (50); and a controller for selectively activating the resistive heating elements (50) on each of the plurality of heating panels (48).
摘要翻译：用于对入口空气过滤器室部件（42）和压缩机结冰敏感的燃烧涡轮的电阻加热系统包括布置在基本上平面的阵列（46,47）中的多个加热板（束）（48），适于定位在涡轮机的入口空气过滤器室（42）上或附近。每个加热板（48）设置有一个或多个电阻加热元件（50）; 以及用于选择性地激活多个加热板（48）中的每一个上的电阻加热元件（50）的控制器。

9. 发明公开

EP2345805A1 Inlet air heating and cooling system for the compressor of a gasturbine 审中-公开
标题翻译： Einlassluftheiz- und-kühlsystemfürden Kompressor einer Gurburbine
公开(公告)号：EP2345805A1
公开(公告)日：2011-07-20
申请号：EP09177609.6
申请日：2009-12-01
申请人： General Electric Company
发明人： Motakef, Abbas , eher, Peter
IPC分类号： F02C6/18 , F02C7/047 , F02C7/08
CPC分类号： F02C7/143 , F02C6/14 , F05D2260/20
摘要： A heating and cooling system (100) for inlet air of a turbine compressor (20). The heating and cooling system (100) may include a fluid coil (120) positioned about the turbine compressor (20) and a thermal energy storage tank (170). The fluid coil (110) and the thermal energy storage tank (170) are in fluid communication such that fluid is both provided to the fluid coil (110) from the thermal energy storage tank (170) for exchanging heat with the inlet air and returned to the thermal energy storage tank (170) without further heat exchange.
摘要翻译：一种用于涡轮压缩机（20）的入口空气的加热和冷却系统（100）。加热和冷却系统（100）可以包括围绕涡轮压缩机（20）定位的流体盘管（120）和热能储存罐（170）。流体线圈（110）和热能储存罐（170）处于流体连通状态，使得流体从热能储存箱（170）向流体线圈（110）提供，用于与入口空气交换热量并返回到热能储存罐（170），而不需要进一步的热交换。

10. 发明公开

EP2180165A2 A system and method for changing the efficiency of a combustion turbine 失效转让
标题翻译：系统和Verfahren zurEffizienzänderungeiner Verbrennungsturbine
公开(公告)号：EP2180165A2
公开(公告)日：2010-04-28
申请号：EP09173219.8
申请日：2009-10-16
申请人： General Electric Company
发明人： Feher, Peter , Motakef, Abbas
IPC分类号： F02C7/047
CPC分类号： F02C7/047 , F01K23/10 , F02C1/05 , F02C6/08
摘要： An embodiment of the present invention takes the form of an application and process that incorporates an external heat source (140) to increase the temperature of the airstream entering a compressor section (155) of a combustion turbine (150). An embodiment of the present invention may perform an anti-icing operation that may not require an Inlet Bleed Heat system (IBH) (125) to operate. An embodiment of the present invention may perform an anti-icing operation that may allow for the IGV angle to remain nearly constant. An embodiment of the present invention may increase the output and efficiency of a combustion turbine (150) operating at partload by delaying IBH operation and delaying the closing IGVs.
摘要翻译：本发明的一个实施例采用了包括外部热源（140）以增加进入燃气轮机（150）的压缩机部分（155）的气流的温度的应用和过程的形式。本发明的实施例可以执行防冰操作，其可以不需要入口放热加热系统（IBH）（125）来操作。本发明的一个实施例可以执行防冰操作，其可以允许IGV角保持几乎恒定。本发明的一个实施例可以通过延迟IBH操作并延迟闭合IGV来增加在部分负载下工作的燃气轮机（150）的输出和效率。

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